View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 25261U 26074.31971367 +.00000000 +00000-0 +15622-3 0 00004
2 25261 98.8254 103.0477 0004213 54.9716 305.1864 14.36275202 07
| Epoch (UTC): | 15 March 2026 07:40:23 |
| Eccentricity: | 0.0004213 |
| inclination: | 98.8254° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 103.0477° |
| argument of perigee: | 54.9716° |
| revolutions per day: | 14.36275202 |
| mean anomaly at epoch: | 305.1864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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